Optical steering element and method

ABSTRACT

A 1×N wavelength selective switch which can function as a dynamic channel equalizer when N=1. In an exemplary arrangement, the present invention is a free-space device that includes a linear array of micromachined reflective elements for beam steering of individual wavelength channels. In at least some embodiments the array of reflective elements of the present invention provides a substantially seamless design such that the optical spectrum appears flat across the transition between actuators. Various embodiments provide high channel bandwidth with flat-top channel performance, low polarization dependence loss, low vibration sensitivity, extinction ratios greater than 40 dB over all temperatures, and very low levels of electrical and optical channel cross-talk.

RELATED APPLICATIONS

This application is related to the following U.S. Patent Applications,which are incorporated by reference as though forth in full herein: Ser.No. 10/059,900; filed Jan. 28, 2002, SYSTEM AND METHOD FOR DYNAMICSPECTRAL CONTROL FOR OPTICAL NETWORKS, filed on or about Jan. 29, 2002;Ser. No. 60/359,167; filed Feb. 20, 2002, System and Method for SeamlessSpectral Control; Ser. No. 10/371,907; filed Feb. 20, 2003, System andMethod for Seamless Spectral Control; Ser. No. 09/549,781; filed Apr.14, 2000 Dynamic Spectral Shaping for Fiber-Optic Application.

FIELD OF THE INVENTION

The present invention relates generally to optical devices, and moreparticularly relates to arrays of steering elements for opticalapplications, including but not limited to Dense Wavelength DivisionMultiplexed (DWDM) systems and Dynamic/Reconfigurable Optical Add/DropModules (OADM), systems which include such arrays, methods forperforming such optical switching, and processing methods forfabricating such devices.

BACKGROUND OF THE INVENTION

Dynamic channel equalizers and wavelength selective switches areconsidered necessary and highly cost-effective building blocks forimplementing dynamic wavelength channel equalization, blocking, andswitching functions in next generation long haul and metro networks.

A favorite device architecture used in these designs is one thatdemultiplexes the spectral content of the input light signal into anarray of wavelength channels using a free-space diffraction grating.Once separated, each wavelength channel can be modulated or redirectedalong a different optical path by an intermediate array of controlelements. After being manipulated, each of the wavelength channels canbe multiplexed back together into one or several output ports by foldingthe path of the light back upon the same grating or directing the pathof light onto another grating of equal dispersion.

When a single fiber optic input and output port is used, the devicefunctions as a dynamic channel equalizer or wavelength blocker. When thelight from individual wavelength channels can be redirected toward anyof N output ports the device functions as a 1×N wavelength selectiveswitch.

One means known in the prior art for the intermediate manipulation ofwavelength channels is to use an array of liquid crystal modulators.Such modulators usually function by changing the polarization state ofeach wavelength channel and can be used to form a wavelength blocker ora 1×2 wavelength selective switch. While it is possible to extend thisapproach to higher port counts, this approach is very costly andcomplicated.

A simpler and more extendible approach to higher port count wavelengthrouting is to use an array of micromachined reflective mirrors forindividual wavelength channel manipulation. Some approaches forachieving this include a mirror array which routes light in eachwavelength channel by either changing the angle of the return opticalbeam or by displacing the path of the return optical beam using mirrorsin a paired plane configuration or a paired retro-reflectorconfiguration.

While such wavelength selective switching is extensively mentioned inthe prior art, a design for implementing both switching as well asequalization has proven to be neither a simple nor an obvious extensionof that art, from a control and design standpoint. In addition to theseconsiderations, the prior art has failed to address adequately otherperformance criteria including high channel bandwidth with flat-topchannel performance, low polarization independence loss, low vibrationsensitivity and therefore high resonant frequency steering elements,high extinction ratios greater than 40 dB, and very low levels ofelectrical and optical channel cross-talk.

Furthermore, some DWDM applications require wavelength selectiveswitching with seamless optical performance in the spectral region inbetween adjacent wavelength channels with frequency spacing typicallyset at 50 GHz or 100 GHz on the ITU grid. Whereas present liquid crystalmodulator arrays offer seamless spectral performance in the non-blockingstate, micromachined arrays of actuators typically have dips ininsertion loss in between the actuator channels. In these regionschromatic dispersion and polarization depended loss (PDL) are oftenuncontrolled. The existence of the dips also reduces the effectiveusable bandwidth associated with each actuator and impose the limitationthat each actuator must have a one-to-one correspondence to eachwavelength channel. This can limit the flexibility of such a device whenlarger or smaller spectral spacing is required. While a wavelengthblocker based upon diffractive micromachined ribbon elements does offerseamless performance across the telecom spectral band, it is difficultto build a wavelength switching device with higher port counts (N>1)based upon this technology, as it is difficult to collect light from thehigher order diffracted modes and redirected in an efficient manner intoadditional ports with low insertion loss.

Thus a new type of actuator array is needed which can efficientlyredirect spectrally separated light towards multiple output ports withnear spectrally seamless performance.

SUMMARY OF THE INVENTION

The present invention provides a 1×N wavelength selective switch whichcan function as a dynamic channel equalizer when N=1. In an exemplaryembodiment, the switch of the present invention is a free-space devicethat includes a linear array of micromachined reflective elements forbeam steering of individual wavelength channels.

Furthermore, in at least some embodiments the array of reflectiveelements of the present invention provides a substantially seamlessdesign; that is, the portion of the spectrally separated light beamimpinging on the gap between two adjacent actuators gets redirected tothe same output position with the same level of attenuation as thespectral component which lands directly on adjacent actuators positionedto the same angle. Thus the optical spectrum appears flat across thetransition between actuators.

To achieve the foregoing, particular attention has been paid to theoptical design and the micromechanical elements for steering the lightbeam. As a result, the design of the present invention provides, in atleast some embodiments, beam steering elements that provide high channelbandwidth with flat-top channel performance, low polarization dependenceloss, low vibration sensitivity, extinction ratios greater than 40 dBover all temperatures, and very low levels of electrical and opticalchannel cross-talk.

THE FIGURES

FIG. 1A is a schematic diagram of an exemplary embodiment used forforming a dynamic channel equalizer and/or a wavelength selective switchwith equalization and blocking capabilities.

FIG. 1B is a detailed side view of Subassembly 1 shown in FIG. 1A

FIG. 1C is a detailed side view of Subassembly 2 shown in FIG. 1A.

FIG. 2 is a schematic diagram of another exemplary embodiment used forforming a wavelength selective switch with equalization and blockingcapabilities.

FIG. 3A is a top view showing an exemplary arrangement of one aspect ofthe present invention in which interdigitated electrode fingers arefolded parallel to the axis of rotation. The stator electrode fingersare arranged in an antenna shape and the rotor fingers surround thestator fingers.

FIG. 3B is an isometric view of the electrode arrangement of FIG. 3B andillustrates the vertical offset between the stator and rotor fingers inone illustrative embodiment.

FIG. 4 is a top view depicting the concentration of electric field linesfor the embodiment shown in FIGS. 3A-3B.

FIG. 5 illustrates an alternative comb finger design.

FIGS. 6A and 6B illustrate aspects of the alternative design shown inFIG. 5, wherein FIG. 6A shows antenna shaped rotor fingers and FIG. 6Bshows claw shaped stator fingers.

FIG. 7 is another alternative embodiment to the design shown in FIGS. 2and 5 in which the stator fingers are electrically connected to eachother by a lower trace of electrically conducting material.

FIG. 8 is side view depiction of the change in gap between the rotor andthe stator fingers during rotation.

FIG. 9A shows a single actuator with a hinge folded around supportingposts. (The comb figures at the end of the actuator are outside thedrawing area).

FIG. 9B is an enlarged illustration of the hinge and post region shownin FIG. 9A.

FIG. 10 is a top view showing an array of micromechanical steeringelements with folded hinges in accordance with one aspect of the presentinvention.

FIG. 11 is a top view of an exemplary embodiment of a hinge designfolded around a supporting post and used to place actuators adjacent toeach other.

FIG. 12 illustrates one example of how the array of FIG. 10 can beextended to very large numbers of closely spaced actuators.

FIG. 13 depicts the top view of an alternative hinge design with asimilar application to the preferred embodiment shown in FIG. 11.

FIG. 14 illustrates a “stopper” placed near the end of the actuator torestrict lateral motion of the actuator during manufacturing processesand lateral shock testing by constricting the available space.

FIG. 15 illustrates an array of actuators with their associated nubs forrestricting lateral motion

FIG. 16A shows an illustrative arrangement of a contiguous array ofnon-seamless actuators

FIG. 16B shows an illustrative arrangement of a contiguous array ofseamless actuators.

FIGS. 17A-I illustrate the process for forming an actuator array.

FIG. 18 shows an outline of the entire process flow.

FIG. 19 shows an internal elevational view of a finished steeringelement with a liquid crystal cell sandwiched between the glass waferswhich are monolithically bonded to this steering element so that lightcan be independently blocked in strength while it is steered in angle.Optionally, a thin sheet polarizer can be placed above or below theliquid crystal.

FIG. 20 shows in schematic diagram form a representation of the outputspot location of the light as its path is steered between ports 1 and 4.A hitless path requires the ability to steer the light along twoorthogonal directions in order to avoid ports 2 and 3.

FIG. 21 depicts a top view of a steering element with the capability tosteer light along both θ_(x) and θ_(y) angular directions

FIG. 22 schematically depicts how motion in the θ_(y) direction of thecentral reflector is achieved

FIG. 23 is an isometric view illustrating how motion along the θ_(x)direction is achieved.

FIG. 24 depicts three biaxial steering elements placed contiguously nextto each other.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

The present invention overcomes many of the limitations of the prior artby providing a substantially integrated solution for dynamicallyattenuating, spectrally equalizing, and switching individual wavelengthson the ITU grid using a free space, optically transparent architecture.In addition, the present invention provides ready expandability forachieving dynamic control with increasing channel counts and bandwidthrequirements. In particular, these features are illustrated in thecontext of an embodiment of the invention in a 1×N channel-based opticalswitch capable of increased channel count operation and equalizationwithout significant operational impairment.

In addition, the present invention provides a set of actuators that areso closely spaced, they have very little residual interchannel dips inthe frequency domain and in at least one embodiment may allow seamlessoperation in the frequency domain. In other words, at least someembodiments of the present invention provide a system where, if everyactuator were set to produce the same attenuation, the entireattenuation spectrum would be flat. Such a seamless system makes theeffects of dead space inconsequential and reduces or eliminates concernsabout pixelation.

Referring first to FIGS. 1A-1C, a generalized top plan view of oneembodiment of a system according to the present invention can beappreciated where that system can be used as a free-space dynamicchannel equalizer or wavelength selective switch. In particular, FIG. 1Aillustrates an exemplary system 100 comprised, for purposes ofdiscussion only, of two subassemblies 101 and 102. The system 100includes an input in the form of a 1×N collimator array 105,polarization control optics 110, a wavelength dispersion device 115 suchas a diffraction grating, an achromatic lens 120, and a steering elementarray 125. In addition, in some embodiments it may be desirable toinclude a telescopic beam expander 130, and/or an anamorphic beamexpander 135, and possibly a turning mirror 140, which functionsprimarily to reduce the physical length of the device relative to thelength of the optical path. The turning mirror 140 may be angle adjustedover temperature, such as disclosed in co-pending U.S. patentapplication Ser. No. 10/915,524, filed Aug. 9, 2004, entitled HeatActuated Steering Mount for Maintaining Frequency Alignment inWavelength Selective Components for Optical Telecommunications, ExpressMail Label No: EV382010549US, commonly assigned and incorporated in fullherein by reference. The steering element array 125 may be, for example,a micromachined linear array of reflective elements for beam steering ofindividual wavelength channels.

Referring particularly to FIG. 1B, this diagram shows a side view ofsubassembly 101. A 1×N array of optical ports 105 can function as aninput or an output port and is shown as a 1×4 array for illustrativepurposes only. The optical signal from each of these ports first passesthrough polarization conditioning by means of polarization controloptics 110, and optional beam expansion optics 130. This yields aseparate output path 145A-D for each beam, at which point the beams arefully conditioned and are passed to subassembly 102, shown in FIG. 1C.Then, each beam is separated into individual wavelengths using adiffraction grating 115. After being separated, the individualwavelength channels are collimated and focused by means of lens 120 ontoan array of steering elements 125. As shown in FIG. 1C, such steeringelements 125, discussed in greater detail hereinafter, allow theindividual wavelength channels to be redirected to any one of the outputoptical ports.

FIG. 2 shows an alternative embodiment to FIG. 1 where the diffractiongrating used is a transmission volume phase diffraction grating 215 withtwo prisms 216 attached to the input and output faces of the grating.Such gratings offer an advantage in some embodiments because they can bemade with high efficiencies for both polarizations. Polarizationdependent loss from the grating can further be reduced by using aquarter-wave plate 220 to rotate incoming and outgoing polarizations by90 degrees after a double pass through the quarter-wave plate. Thiseliminates the need for the separate polarization control optics 110discussed in connection with FIG. 1. Because the input path length ofthe light from the collimator array to the grating can be made muchshorter in this design, the telescopic beam expander 130 shown in FIG. 1can be eliminated. An anamorphic beam expander 235 is still useful insome embodiments to achieve high spectral resolution. However, thedependence of a volume phase grating line count with temperature and theindex of refraction change of the prisms with temperature leads to muchmore temperature dependence of the grating-prism system. A turningmirror 240, whose angle can be controlled as a function of temperatureto change the input angle of light into the grating, can compensate forthese effects. The mount and mirror arrangement disclosed in theabove-referenced U.S. Patent Application Ser. No. 10/915,524, filed Aug.9, 2004, entitled Heat Actuated Steering Mount for Maintaining FrequencyAlignment in Wavelength Selective Components for OpticalTelecommunications, Express Mail Label No: EV382010610US, is suitablefor this purpose.

It has been determined that performing both equalization and switchingfunctions simultaneously requires special attention to both the designof the micromechanical elements and the spacing of the input/outputfibers of a 1×N port array. One means of providing equalization is toadjust the path of the return light so that the return Gaussian beam isshifted slightly so as to reduce the overlap with the optimized paththereby providing additional loss and a means of attenuating the signal.This solution requires smooth drift free continuous analog control ofthe steering elements that is controlled with a high bit count DAC.

Over the length of the actuation array, it has been determined that itis desirable to have as little optical dead space as possible betweenindividual adjacent actuators corresponding to each wavelength channel.Reducing this dead space maximizes the useful bandwidth for sending 10Gbits/s or even 40 Gbits/s data through each channel as well as reducingthe frequency alignment tolerance of optical sources to the ITU grid.Therefore, in order to build an efficient DWDM system, it has been founddesirable to have this optical dead space correspond to a small fractionof the total bandwidth separating adjacent channels on the ITU grid.

However, as the size and spacing of adjacent actuators is reduced,adjacent elements become more susceptible to cross talk. For bestperformance, cross talk should be minimized between adjacent channels sothat data traveling on adjacent channels do not interfere. When channelsare close together, dynamic interference from squeeze film air/nitrogendamping is an important issue. To eliminate the effect of squeezed filmair damping, transitions in the drive voltages are, for at least someembodiments, slowed down to a rate less than the natural time constantof the micromechanical steering elements. Slowing the actuators down hasthe added benefit of dramatically reducing overshoot and ringingeffects. Correspondingly, it has been found to be helpful to designsteering elements with a high mechanical frequency because thisfrequency limits the switching speed. Another reason it is useful forthe steering elements to have a high resonant frequency is to improvetheir immunity from opto-mechanical noised generated by in-situvibrations. It has also been found desirable, for improved performanceof the array of steering elements, to include uniformity in theactuation response across the array, as well as minimization ofhysteretic behavior, drift over temperature, and aging effects.

FIGS. 3A and 3B illustrate in plan view and isometric view,respectively, an exemplary arrangement of a steering element inaccordance with one aspect of the present invention in which a statorcomb indicated generally at 300 is arranged as a plurality of statorelectrode comb fingers 305. The fingers 305 are organized in an“antenna” geometry such that the stator electrode comb fingers lieprincipally parallel to the hinge of rotation, shown in FIG. 3A at 310,and are interdigitated with a plurality of rotor electrode comb fingers315 which are formed integrally with a reflective element 320. Thetorsional hinges 310 can be seen to be attached substantially at thecenterline of the reflective element 320. As shown in FIG. 4, thisarrangement of stator electrode fingers 305 and rotor electrode combfingers 315 confines the majority of the in-plane electric field lines400 along the x-axis so that very little if any forces are present alongthe y-axis, thus minimizing the risk of lateral twisting.

An alternative embodiment to forming the “antenna” geometry along thestator electrodes is shown in FIG. 5 and FIG. 6, where the “antenna”structure 505 is formed on the rotor, with an interdigitated stator 510,with the remaining elements the same as shown in FIGS. 3A and 3B. Afurther alternative embodiment is shown in FIG. 7 where vertical statorteeth 705 are formed to be disposed within rotor orifices 710. Theembodiments shown in FIGS. 5-7 are also desirable because they furtherlimit cross talk from the fringing electric fields.

It can be appreciated from each of the foregoing alternativearrangements that the interdigitated portions—the stators and therotors—are situated substantially in a direction parallel to thetorsional hinge and the axis of rotation of the reflective element.Stated differently, one aspect of the present invention is the use of aninterdigitated arrangement of electrodes for providing the capacitiveforces necessary for angular rotation of the elements and which do notpresent the lateral snap-in phenomenon characteristic of at least someof the prior art. These embodiments of the present invention also havethe benefit that they do not require the use of a self-alignmentprocess.

As shown in FIG. 8, which illustrates the reflective element 800 and itshinge 805 in cross-sectional side view, at least certain arrangements ofthe present invention minimize the problem of mechanical interferencebetween the interdigitated rotor and stator electrodes 810 and 815,respectively, at least for the small angles of rotation characteristicof such devices. More specifically, the reflective element 800 islimited in its range of motion a physical stop such as the substrate820, before any portion of the rotor 810 can contact the stator 815,while still permitting actuation of up to several degrees of tilt.

A useful aspect of at least some embodiments of the invention is a highfill percentage. Stated differently, this aspect provides a decrease inthe optical dead space in between each channel in order to increase thetotal spectral bandwidth associated with each wavelength channelimpinging upon the micro steering array. This aspect can be appreciatedfrom the hinge geometry shown in the FIGS. 9A-9B and 10, whichillustrates an exemplary arrangement for at least some embodiments. Inthe arrangement of FIGS. 9A-9B and 10, hinges 910 are attached to theoutside edges 915 of a post 920. Here the post 920 refers to the areaused to anchor the steering element 925 to the substrate 930, withessentially symmetrical reflective steering areas 935 on either side ofthe post 920 in the illustrated embodiment, although such symmetry isnot required in all embodiments. This geometry allows the steeringelements 925 to be placed continuously in a single line (see FIG. 10)while minimizing the space taken up by the hinge 910 and the supportingpost 920. This hinge design enables the posts 920 to be shared betweenadjacent steering elements 925 as shown in FIGS. 10 and 11 which in turnallows a large numbers of actuators, or steering elements, 925 to bespaced contiguously in a small area as shown in FIG. 12. An alternativehinge design is shown in FIG. 13 where the hinges 1310 intersect acentral bridge point 1315 between two posts 1320. Steering elements witha linear fill factor as large as 98% have been achieved with both of thehinge post-sharing geometries depicted in FIG. 11 and FIG. 13.

Another beneficial aspect of some embodiments of the present inventionis the use of a carefully placed lateral “stopper” 1410 as shown inFIGS. 14 and 15 The purpose of the lateral stopper 1410 is to limit thelateral motion of the mirrors, or steering elements, 1415 during extrememechanical shock testing or sudden pressure changes that may occurduring unloading or loading wafers from a low pressure etchingapparatus. Such pressure changes expose steering element and the end ofthe ends of rotor combs 1416 to a high degree of mechanical shock. Inaddition, these lateral stops 1410 provide an extra layer of safety bypreventing stiction between adjacent actuators 1415. The distance 1420between the stopper and wall is typically chosen to be less than orequal to the gap 1425 between adjacent steering elements 1415. In atleast some embodiments, the use of such stoppers is helpful in providinga high yield, low cost design. It will be appreciated that, while thelateral stoppers 1410 are illustrated as formed external to the steeringelements 1415, in at least some embodiments the stoppers 1410 couldinstead be formed on the steering elements.

Another aspect of the present disclosure, is that at least someembodiments of the invention are compatible with a diffractive steeringapproach that has seamless operation as discussed in U.S. patentapplication Ser. No. 10/371,907; filed Feb. 20, 2003, by Stowe et al.entitled System and Method for Seamless Spectral Control. In adiffractive steering approach, slots 1600 (only some of which aredesignated by a reference numeral for the sake of clarity) are cut intothe array of steering elements 1610 as shown by a comparison of FIGS.16A-16B, where FIG. 16A illustrates the steering elements 1610 in asimple arrangement while FIG. 16B illustrates the steering elements 1610configured to operate as seamless diffractive application by theaddition of the slots 1600. These slots 1600 are arranged to form aperiodic amplitude grating which masks the transitions between channels,so that a Gaussian beam with a spot size larger than the period of theslot pattern will experience no optical transition in phase between twoadjacent reflective elements actuated to steer the reflected light tothe same output port with the same equalization. One aspect ofdiffractive steering is that, preferably, no electrical lines orstructural connection should be underneath the reflective region unlessthose lines or connections are also periodic at the same frequency asthe slot pattern. Thus, one advantage of this aspect of the invention isthat none of the electrical signals needed to actuate the steeringelements have traces underneath the reflective region. Instead thesetraces may be routed solely to the outside interdigitated electrodes.The seamless approach allows a customer to group adjacent channels intooptical sub-bands for added system flexibility. In addition this designallows seamless operation to be extended to 1×N wavelength switchingdevices, as desired for the particular implementation.

FIGS. 17A-17I, taken together with the process flow diagram of FIG. 18,show an exemplary set of fabrication steps for manufacturing oneimplementation of a micromechanical array in accordance with the presentinvention, for example that shown in FIG. 12. More specifically, FIG. 17A is a side view of a silicon-on-insulator (SOI) wafer 1700. Such awafer 1700 serves as the starting material for forming a linear array ofmicromachined reflective steering elements in accordance with thepresent invention. Such a silicon on insulator wafer comprises a buriedoxide layer 1705 that is positioned above a substrate 1710 and beneath atop silicon layer 1715.

Referring next to FIG. 17B, a recess 1720 is patterned into the topsilicon layer 1715 using a deep RIE etch that is masked bylithographically defined photoresist 1719. This recess 1720 is usedlater to form an electrical contact to the stator combs that are used todrive a steering element. Next, as shown in FIG. 17C, the SOI wafer 1700is oxidized, creating layer 1725. The layer 1725 provides insulationduring subsequent fusion bonding. Next, FIG. 17D shows the result whenphotoresist 1736 is lithographically exposed and this pattern istransferred into the top silicon layer using deep RIE. This patterndefines the channel posts 1730, stator combs 1735, and drive trace area1740, as well as forming a cavity 1741 underneath each of the steeringelements (as yet to be formed). In addition, a separate hole 1742 may becut on the left side to allow a front side electrical contact to thebottom silicon 1710.

Next, as shown in FIG. 17E, another SOI wafer 1745 is fusion bonded tothe patterned SOI wafer 1700, after which the top SOI handle wafer andburied oxide layer have been removed, as shown in FIG. 17F. This leavesa thin silicon membrane 1750 bonded to the bottom, and now patterned,SOI wafer 1700. Then photoresist is lithographically patterned and thispattern is transferred to the top silicon membrane 1750 and theunderlying oxide using deep RIE. As shown in FIG. 17G, this defines thetop steering elements 1755 together with their rotor combs 1760.Additional hole 1765 is opened to allow electrical access to the siliconground plane 1710 as well as holes 1766 to the underlying stator combs1735 used to drive each steering element 1755. Thereafter, thephotoresist is removed with an O₂ plasma etch.

Next, FIG. 17H shows the shadow mask 1770 used to confine deposited bondpad metallization 1775 to the bond pad regions 1780. Finally, (FIG. 17I)a thin layer of reflective metal 1785 is deposited over the steeringelements 1755 using another shadow mask 1790.

FIG. 18 illustrates a simplified process flow for building the structureshown in FIGS. 17A-17I. The process of FIG. 18 starts at step 1800 witha silicon-on-insulator (SOI) wafer. At step 1805, bond pad recesses areformed by means of lithography and etch. Then, at step 1810, initialoxidation occurs. At step 1815, the bottom stator, mechanical posts, andelectrical traces are formed using lithography and etch techniques(oxide, silicon, oxide), followed at step 1820 by bonding of the upperSOI wafer, followed by an anneal. Next, at step 1825, the top handlewafer is etched away (see FIG. 17F) to remove the silicon and the oxide.At step 1835, the reflective elements and rotors are formed by means oflithography and etch processes (removal of silicon and oxide).Alternatively, a hard oxide mask may be used to form the reflectiveelements and rotors, wherein a masking oxidation is performed at step1830, after which at step 1836 the reflective elements and rotors areformed by means of lithography and etch processes (again, removal ofoxide, then silicon, then more oxide), and then at step 1840 an oxideetch is performed to remove the masking oxide. At step 1845 metal isevaporated and annealed to form bonding pads. Finally, at step 1850 thereflective metal layer is evaporated onto the appropriate regions (FIG.17I). The process of FIG. 18 is then complete; however, those skilled inthe art will recognize that different processing approaches may be usedto yield the same structure, and thus this process is merely exemplaryfor one implementation of the structure of the present invention.

Referring briefly to FIG. 1C, it will be appreciated by those skilled inthe art that, during the transition from switching a channel from port 1to port 4, there is an intermediate point at which the light beam mightpass through ports 2 and 3. In such event, a small transient signalwould be seen in ports 2 & 3 when switching from ports 1 to 4. In somecases such transient effects can compromise the system architecture of anetwork system vendor. Thus a “hitless” means of switching between ports1 and 4 is desirable such that no transient signals are seen in ports 2or 3.

One possible means for providing hitless functionality involvesattenuating the reflected amplitude of each wavelength channel duringthis transition. To achieve this, a liquid crystal array may be mountedon top of the micromechanical steering element array. FIG. 19 shows anexemplary arrangement for monolithically integrating a liquid crystalarray 1910 for the purpose of attenuation during a switching event.Typically, this liquid crystal array 1910 is of the twisted nematic typewith a thin sheet polarizer 1915 mounted either on the top or bottom ofthe stack. In addition, the cell sizes for each channel arelithographically matched in size to the spacing of micromechanicalsteering elements. In this embodiment, the liquid crystal elements 1910can be bonded to the array of micromechanical steering elements with asmall air gap 1920 by means of bonding posts 1925, with a transparentITO electrode 1930 formed adjacent the liquid crystal array 1910 and anAR coated capping wafer 1935 positioned at the top of the stack. Atypical substrate material for the liquid crystal array would be onesuch as Corning Pyrex 7740 or Borofloat (manufactured by Shot Glass)because their coefficients of thermal expansion are directly matched tosilicon. Additionally, the preferred embodiment would try to minimizethe total stack height between the liquid crystal and steering elementarray in order to keep the elements within the Rayleigh range of thecollimated Gaussian beam of light impinging on each channel. While theabove-described structure works in principle, it requires a complicatedsystem of alignment and complicated routing of two sets of drivesignals, one set for the liquid crystal array and one set for themicromechanical steering elements.

A simpler method for implementing hitless operation is to form an arrayof biaxial steering elements that can be tilted along the axisperpendicular to the length of the array (hereinafter the “θ_(x)”direction). As depicted in FIG. 20, the effect of tilting the steeringelements along this direction is to cause the return path of the lightto be laterally displaced along the direction transverse to the array ofoutput fibers. Thus, when a beam is redirected from output port 1 to 4(labeled as elements 2005 and 2020 respectively) by changing thesteering element angle along θ_(y), the beam can also be simultaneouslydisplaced laterally by tilting the MEMS steering element along the θ_(x)direction such that the beam misses the intermediate port 2 and port 3(labeled as elements 2010 and 2015 respectively). The hitless path ofthe return beam takes during switching is shown as the dotted line 2000.Thus, hitless operation can be accomplished by simultaneously steeringlight along orthogonal angular directions θ_(x) and θ_(y) in a singlelinear array. In some cases the tilt necessary to achieve hitlessperformance along the perpendicular θ_(x) direction may be as much asfive degrees.

Such a micromechanical design is challenging if the requirement for ahigh fill factor is maintained, as it may be in at least someembodiments. FIG. 21 illustrates a top view of a steering element 2100designed to tilt along both θ_(x) and θ_(y) directions simultaneously.This design eliminates the need for complicated routing underneath thereflective steering elements. In this arrangement, the steering element2100 is made from a central reflective mirror element 2110 mechanicallylinked to two outside steering actuators 2120 and 2121 by four flexuraljoints 2140, 2141, 2142 and 2143. Both surrounding actuators have asimilar arrangement of stator and rotor comb geometry as describedearlier in FIG. 6 and can be constructed by process steps similar tothose described in FIGS. 17 and 18. In addition, in an exemplaryarrangement, the steering actuators may use all of the design pointsconcerning the folding of hinges around the posts as described inconnection with FIGS. 9-13. The four flexural joints 2140-2143 compriseserpentine mechanical linkages that are primarily compliant enough toallow angular twisting along θ_(y) between the central reflective mirrorand the outside steering actuators. It is advantageous, in at least someembodiments, to make these linkages thin enough so that the centralreflector experiences no warping during actuation. Because the θ_(y)steering actuators are joined to the central reflective mirror in thiscompound configuration, the angular range of motion of the centralmirror can be magnified along the θ_(y) direction by choosing theappropriate arm lengths of the central reflector and surroundingtorsional actuators. For this to occur, the motion of both actuators2120 and 2121 are driven in the same direction in the illustratedarrangement. Such motion is depicted from the side view in FIG. 22 wherethe linkages are shown in their relaxed 2240 and unrelaxed states 2240′.All four linkages are assumed thin enough to flex without causingwarping in the central reflector region 2210. By torsionally pulling onboth outside actuators 2220 and 2230 about their respective hinges 2250and 2260, the central reflector is twisted about θ_(y).

An additional aspect of the four linkages is that they can be thermallyactuated to provide a twisting mechanism for motion θ_(x). In order toaccomplish this motion, which may be desirable in some embodiments, aone-to-two micron thick metal layer is shadow mask deposited on top ofall four flexural linkage joints. It is possible to put this layer downat the same time that aluminum is put down for the bond pad connectionsdiscussed in FIG. 17H. This evaporated metal forms a bimorph structurethat allows out-of-plane movement to occur at these linkages when theyare heated to a different temperature. Finally, a highly conductive pathmay be formed along the dashed line originating at 2160 and terminatingat 2165. This path may, for example, be created by ion implantationbefore the mirror regions and top rotor combs are cut. The purpose ofthis path is allow a current to flow predominately through the top twolinkages 2142 and 2143; thus heating the top two linkages more than thebottom two linkages 2140 and 2141, causing a larger out-of-planedisplacement in the top two linkages as compared to the bottom twolinkages. Because heat is initially concentrated on these top linkagesthere is a differential change in the curvature of the top linkages overthe bottom linkages. This then leads to a twisting motion in the centralsteering element as best depicted in the isometric view shown in FIG.23. Here 2310 shows the relaxed state of the mirror and 2310′ shows theenergized state with current flow on and current flowing predominatelythrough the top two linkages 2322 and 2323. The four linkages 2320,2321, 2322, and 2323 are drawn with a smaller number of folds than shownin FIG. 21 for visual clarity. Once this current is turned off heatdiffuses through the entire structure causing the central steeringelement to return to its equilibrium position. Simple modeling showsthat the time constant for tilting the reflective element along theθ_(x) direction is limited by the thermal time constant for heat todiffuse down the legs. Designs can be easily achieved which operate withless than 20 degrees Celsius increase from ambient temperature, a fewmilliseconds of switching time, and with less than 1 mW of input power.Finally, the symmetry of the structure eliminates changes in tilt alongθ_(x) to changes in the background temperature as no tilt is induced ifboth the top and bottom linkages are at the same temperature. Becausethe steering element structure has geometric symmetry it can be designedto balance moments of inertia so there is no net torque about the centerof mass due to mechanical shock and external vibration along all threeorthogonal axes.

FIG. 24 shows three biaxial steering elements placed next to each other.In a typical arrangement, the torsional actuators at each end may beconstructed using the design elements and process flow already disclosedin this invention, although it will be appreciated by those skilled inthe art that such an approach is not required for all embodiments. Eachof the right most comb drive actuators 2461, 2462, and 2463 (to theright of the central reflective elements 2410, 2420, and 2430) can shareadjacent posts 2471 and 2472 and a common input current path 2240. Anelectrical switch such as an analog demultiplexer can be used toselectively open or close the individual output current paths 2450,2451, and 2452 of each individual steering element. It will be apparentto those skilled in the art, given the teachings herein, that additionalelements can be placed next to each other to form a linear array of nsteering actuators capable of steering the light along two orthogonaldirections.

Having fully described an exemplary arrangement and variousalternatives, it will be appreciated by those skilled in the art thatnumerous alternatives and equivalents exist which do not depart from theinvention. It is therefore intended that the present invention not belimited by the foregoing description, but only by the appended claims.

1. A free space 1×N wavelength selective switch comprising: an inputport for receiving an input beam, an output port for transmitting anoutput beam, a grating for separating the input beam into individualwavelengths, at least one reflective element, each reflective elementincluding a stator and having a length and a width, a rotor positionedon a substrate and configured to electrically interact with the statorupon the application of an electrostatic force therebetween, the statorand rotor each having interdigitated elements arranged orthogonally tothe length of the reflective element, optical beam guiding componentsfor receiving the input beam and directing the beam to the at least onereflective element and then to the output port as an output beam,wherein N is equal to 1 and the switch operates as a dynamic channelequalizer.
 2. A free space 1×N wavelength selective switch comprising aninput port for receiving an input beam, an output port for transmittingan output beam, a grating for separating the input beam into individualwavelengths, at least one reflective element, each reflective elementincluding a stator and having a length and a width, a rotor positionedon a substrate and configured to electrically interact with the statorupon the application of an electrostatic force there between, the statorand rotor each having interdigitated elements arranged orthogonally tothe length of the reflective element, optical beam guiding componentsfor receiving the input beam and directing the beam to the at least onereflective element and then to the output port as an output beam,wherein the interdigitated elements on the stator are fingers, whereinthe movement of the reflective element is rotation about an axis and theinterdigitated fingers are oriented parallel to the axis of rotation. 3.A seamless wavelength selective switch comprising an input port forreceiving an input beam, an output port for transmitting an output beam,a plurality of reflective elements, each reflective element including astator and having a length and a width, a rotor positioned on asubstrate and configured to electrically interact with the stator uponthe application of an electrostatic force therebetween, a hingeoperatively affixed to the reflective element and to the substrate topermit the reflective element to move upon the application of anelectrostatic force applied to the stator and rotor, a plurality ofslots in the reflective elements to form a periodic amplitude grating tomask transitions between channels, and optical beam guiding componentsfor receiving the input beam and directing the beam to the linear arrayand then to the output port as an output beam.
 4. The wavelengthselective switch of claim 3 further comprising a plurality of traces forconducting electrical signals wherein the traces are not positionedunderneath the reflective region.
 5. A free space 1×N wavelengthselective switch comprising: an input port for receiving an input beam,an output port for transmitting an output beam, at least one reflectiveelement, each reflective element including a stator and having a lengthand a width, a rotor positioned on a substrate and configured toelectrically interact with the stator upon the application of anelectrostatic force therebetween, the stator and rotor each havinginterdigitated elements arranged orthogonally to the length of thereflective element, a post affixed to the substrate, and a hingeassociated with the at least one reflective element and affixed to thepost to allow the at least one reflective element to move in response toan electrostatic force applied between the stator and the rotor, and,optical beam guiding components for receiving the input beam anddirecting the beam to the at least one reflective element and then tothe output port as an output beam.
 6. The wavelength selective switch ofclaim 5 further comprising a plurality of posts, and a plurality ofreflective elements connected thereto to create a linear array.
 7. Thewavelength selective switch of claim 5 further including a stopper toprevent mechanical interference between the stator and the rotor.
 8. Thewavelength selective switch of claim 5 wherein a single post providessupport for two hinges and their associated reflective elements.
 9. Thewavelength selective switch of claim 8 wherein the reflective elementsare disposed symmetrically about the hinge.
 10. The wavelength selectiveswitch of claim 8 wherein a fill ratio in excess of 90 percent isachieved.